MIL-STD-1553 (original) (raw)
MIL-STD-1553 (kurz MIL-Bus) ist ein Feldbus, den die US-Luftwaffe 1973 einführte.
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| dbo:abstract | MIL-STD-1553 (kurz MIL-Bus) ist ein Feldbus, den die US-Luftwaffe 1973 einführte. (de) MIL-STD-1553 es el estándar militar publicado por el Departamento de Defensa de Estados Unidos que define las características mecánicas, eléctricas y funcionales de un bus de datos en serie. Fue diseñado en principio para su uso en aviación militar, pero ha terminado por utilizarse habitualmente en subsistemas embarcados de manejo de datos en vehículos espaciales, tanto militares como civiles. Proporciona una interfaz física de línea balanceada dual, una interfaz de red diferencial, , protocolo de comando/respuesta half-duplex y hasta 31 terminales remotos. Una versión de MIL-STD-1553, que utiliza cableado óptico en lugar de eléctrico, es conocida como MIL-STD-1773. MIL-STD-1553 fue publicado por primera vez en 1973 como un estándar de la de la U.S. Air Force, y fue utilizado en el avión de combate F-16 Fighting Falcon. Rápidamente le sucedieron otros diseños de aviones, entre ellos el F-18 Hornet y el F-20 Tigershark. Actualmente es ampliamente utilizado por todas las ramas del ejército de Estados Unidos y ha sido adoptado por la OTAN como STANAG 3838 AVS. MIL-STD-1553 está siendo reemplazado en nuevos diseños norteamericanos por FireWire. (es) MIL-STD-1553 est une norme décrivant un bus de communication largement utilisé en avionique militaire et spatiale.Elle a également été adoptée par l'OTAN sous l'appellation STANAG 3838. (fr) MIL-STD-1553 is a military standard published by the United States Department of Defense that defines the mechanical, electrical, and functional characteristics of a serial data bus. It was originally designed as an avionic data bus for use with military avionics, but has also become commonly used in spacecraft on-board data handling (OBDH) subsystems, both military and civil, including use on the James Webb space telescope. It features multiple (commonly dual) redundant balanced line physical layers, a (differential) network interface, time-division multiplexing, half-duplex command/response protocol, and can handle up to 31 Remote Terminals (devices); 32 is typically designated for broadcast messages. A version of MIL-STD-1553 using optical cabling in place of electrical is known as MIL-STD-1773. MIL-STD-1553 was first published as a U.S. Air Force standard in 1973, and first was used on the F-16 Falcon fighter aircraft. Other aircraft designs quickly followed, including the F/A-18 Hornet, AH-64 Apache, P-3C Orion, F-15 Eagle and F-20 Tigershark. It is now widely used by all branches of the U.S. military and by NASA. Outside of the US it has been adopted by NATO as STANAG 3838 AVS. STANAG 3838, in the form of UK MoD Def-Stan 00-18 Part 2, is used on the Panavia Tornado; BAE Systems Hawk (Mk 100 and later); and extensively, together with STANAG 3910 "EFABus", on the Eurofighter Typhoon. Saab JAS 39 Gripen uses MIL-STD-1553B. The Russian made MiG-35 also uses MIL-STD-1553. MIL-STD-1553 is being replaced on some newer U.S. designs by IEEE 1394. (en) MIL-STD-1553는 미국 국방성에 의해 발간되는 군사규격으로 시리얼 통신 데이터 특성을 정의하였다. 이것은 원래 군사용 항공전자 시스템을 위해 설계되었으나 점차 민간 및 군사분야에서 항공기 탑재 장비 데이터 처리에 사용하게 되었다. 이것의 특징은 두 개의 물리적 레이어를 가지고 있다. 1973년 미국 공군에 의해 처음 발간되었으며, F-16 전투기에 처음 사용하였다. 미국 국방 분야에서 넓게 사용하였고, NATO에서도 STANAG 3838 AVS으로 적용하였다. MIL-STD-1553는 현재 파이어와이어(FireWire)로 대체되고 있다. (ko) MIL-STD-1553是美国国防部发布的一个军用标准，定义了机械、电气和串行数据总线的功能特征。它最初是设计來作为军用航空电子的航空数据总线，但现在已普遍用于军用和民用航天器的（OBDH）子系统。它具有多个（通常为双重）的物理层、一个差分、时分多路复用、半双工命令/响应协议，并可处理多达30个远程终端（设备）。使用光缆代替电缆的MIL-STD-1553版本称为MIL-STD-1773。 MIL-STD-1553最早在1973年作为一项美国空军标准发布，并首次用于F-16戰隼戰鬥機战斗机。其他飞机的设计也迅速跟进，包括F/A-18黃蜂式戰鬥攻擊機、AH-64阿帕契直升機、P-3獵戶座海上巡邏機、F-15鷹式戰鬥機以及F-20虎鲨战斗机。它现在在美军所有軍種广泛使用，北大西洋公约组织（NATO）亦已將之作為STANAG 3838 AVS采用。STANAG 3838在英国为UK MoD Def-Stan 00-18 Part 2，使用于龍捲風戰鬥轟炸機、鹰式教练机（Mk 100及之后），以及广泛配合 -“EFABus”，用于颱風戰鬥機。JAS 39獅鷲戰鬥機使用MIL-STD-1553B。俄罗斯制造的米格-35戰鬥機也使用MIL-STD-1553。印度的烈火系列飛彈据称也使用了该总线系统，并还有不少军事装备应用该总线作为电子通信接口。MIL-STD-1553正在由一些更新的美国技术取代，如IEEE 1394。 (zh) MIL-STD-1553 (MIL-STD-1553B) — стандарт Министерства обороны США, распространяется на магистральный последовательный интерфейс (МПИ) с централизованным управлением, применяемый в системе электронных модулей. Принят в СССР в 1987 г. как ГОСТ 26765.52-87 и затем в РФ как ГОСТ Р 52070-2003 «Интерфейс магистральный последовательный системы электронных модулей». Изначально разрабатывался по заказу МО США для использования в военной бортовой авионике, однако позднее спектр его применения существенно расширился, стандарт стал применяться и в гражданских системах. Особенностью интерфейса является двойная избыточная линия передачи информации, полудуплексный протокол «команда-ответ» и до 31 удалённого абонента (оконечного устройства). Каждая линия управляется своим контроллером канала. Стандарт устанавливает требования к: * составу технических средств интерфейса; * организации контроля передачи информации; * характеристикам линии передачи информации (ЛПИ); * характеристикам устройств интерфейса; * интерфейсу с резервированием. Впервые опубликован в США как стандарт ВВС в 1973 году, применён на истребителе F-16. Принят в качестве стандарта НАТО — STANAG 3838 AVS. В новейших самолетах заменяется стандартом IEEE 1394b. (ru) |
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| dbo:wikiPageExternalLink | http://www.altadt.com/support/tutorials/mil-std-1553-tutorial-and-reference/ http://www.amdtec.com.tr/36/military-computer-with-4th-gen-intel-i7-mil-std-1553-canbus-dual-lan-com-usb-30 http://www.aviftech.com/ http://www.ddc-web.com/Documents/dguidehg.pdf http://www.sae.org/technical/standards/AS15531 http://www.sae.org/technical/standards/AS15532 http://www.sae.org/technical/standards/AS4111 http://www.sae.org/technical/standards/AS4112 https://quicksearch.dla.mil/qsDocDetails.aspx%3Fident_number=36973 https://quicksearch.dla.mil/qsDocDetails.aspx%3Fident_number=37131 http://www.aim-online.com/pdf/OVW1553.PDF http://www.mil-1553.com/tutorials-1553 http://www.ballardtech.com/support.aspx/Tutorials/%23mil-std-1553 http://www.pe.gatech.edu/courses/introduction-mil-std-1553 https://apps.dtic.mil/sti/pdfs/ADA202511.pdf https://archive.today/20130411004622/http:/defense.ge-ip.com/library/detail/11743%3Fcid=wik1553 https://web.archive.org/web/20130903081458/http:/aviftech.com/files/3313/5168/8298/1553_Tutorial.pdf https://web.archive.org/web/20160206100357/http:/www.milstd1553.com/ http://quicksearch.dla.mil/qsDocDetails.aspx%3Fident_number=36973 |
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| rdfs:comment | MIL-STD-1553 (kurz MIL-Bus) ist ein Feldbus, den die US-Luftwaffe 1973 einführte. (de) MIL-STD-1553 est une norme décrivant un bus de communication largement utilisé en avionique militaire et spatiale.Elle a également été adoptée par l'OTAN sous l'appellation STANAG 3838. (fr) MIL-STD-1553는 미국 국방성에 의해 발간되는 군사규격으로 시리얼 통신 데이터 특성을 정의하였다. 이것은 원래 군사용 항공전자 시스템을 위해 설계되었으나 점차 민간 및 군사분야에서 항공기 탑재 장비 데이터 처리에 사용하게 되었다. 이것의 특징은 두 개의 물리적 레이어를 가지고 있다. 1973년 미국 공군에 의해 처음 발간되었으며, F-16 전투기에 처음 사용하였다. 미국 국방 분야에서 넓게 사용하였고, NATO에서도 STANAG 3838 AVS으로 적용하였다. MIL-STD-1553는 현재 파이어와이어(FireWire)로 대체되고 있다. (ko) MIL-STD-1553是美国国防部发布的一个军用标准，定义了机械、电气和串行数据总线的功能特征。它最初是设计來作为军用航空电子的航空数据总线，但现在已普遍用于军用和民用航天器的（OBDH）子系统。它具有多个（通常为双重）的物理层、一个差分、时分多路复用、半双工命令/响应协议，并可处理多达30个远程终端（设备）。使用光缆代替电缆的MIL-STD-1553版本称为MIL-STD-1773。 MIL-STD-1553最早在1973年作为一项美国空军标准发布，并首次用于F-16戰隼戰鬥機战斗机。其他飞机的设计也迅速跟进，包括F/A-18黃蜂式戰鬥攻擊機、AH-64阿帕契直升機、P-3獵戶座海上巡邏機、F-15鷹式戰鬥機以及F-20虎鲨战斗机。它现在在美军所有軍種广泛使用，北大西洋公约组织（NATO）亦已將之作為STANAG 3838 AVS采用。STANAG 3838在英国为UK MoD Def-Stan 00-18 Part 2，使用于龍捲風戰鬥轟炸機、鹰式教练机（Mk 100及之后），以及广泛配合 -“EFABus”，用于颱風戰鬥機。JAS 39獅鷲戰鬥機使用MIL-STD-1553B。俄罗斯制造的米格-35戰鬥機也使用MIL-STD-1553。印度的烈火系列飛彈据称也使用了该总线系统，并还有不少军事装备应用该总线作为电子通信接口。MIL-STD-1553正在由一些更新的美国技术取代，如IEEE 1394。 (zh) MIL-STD-1553 es el estándar militar publicado por el Departamento de Defensa de Estados Unidos que define las características mecánicas, eléctricas y funcionales de un bus de datos en serie. Fue diseñado en principio para su uso en aviación militar, pero ha terminado por utilizarse habitualmente en subsistemas embarcados de manejo de datos en vehículos espaciales, tanto militares como civiles. Proporciona una interfaz física de línea balanceada dual, una interfaz de red diferencial, , protocolo de comando/respuesta half-duplex y hasta 31 terminales remotos. Una versión de MIL-STD-1553, que utiliza cableado óptico en lugar de eléctrico, es conocida como MIL-STD-1773. (es) MIL-STD-1553 is a military standard published by the United States Department of Defense that defines the mechanical, electrical, and functional characteristics of a serial data bus. It was originally designed as an avionic data bus for use with military avionics, but has also become commonly used in spacecraft on-board data handling (OBDH) subsystems, both military and civil, including use on the James Webb space telescope. It features multiple (commonly dual) redundant balanced line physical layers, a (differential) network interface, time-division multiplexing, half-duplex command/response protocol, and can handle up to 31 Remote Terminals (devices); 32 is typically designated for broadcast messages. A version of MIL-STD-1553 using optical cabling in place of electrical is known as MIL- (en) MIL-STD-1553 (MIL-STD-1553B) — стандарт Министерства обороны США, распространяется на магистральный последовательный интерфейс (МПИ) с централизованным управлением, применяемый в системе электронных модулей. Принят в СССР в 1987 г. как ГОСТ 26765.52-87 и затем в РФ как ГОСТ Р 52070-2003 «Интерфейс магистральный последовательный системы электронных модулей». Изначально разрабатывался по заказу МО США для использования в военной бортовой авионике, однако позднее спектр его применения существенно расширился, стандарт стал применяться и в гражданских системах. Стандарт устанавливает требования к: (ru) |
| rdfs:label | MIL-STD-1553 (de) MIL-STD-1553 (es) MIL-STD-1553 (fr) MIL-STD-1553 (en) MIL-STD-1553 (ko) MIL-STD-1553 (ru) MIL-STD-1553 (zh) |
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